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弹箭与制导学报 >

2011 , Vol. 31 >Issue 6: 1 - 4

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.06.033

导弹与制导技术

三维自校正制导律的设计与仿真

  • 陈胜琪 ,
  • 周军
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  • 西北工业大学精确制导与控制研究所,西安 710072

陈胜琪(1965-),男,浙江新昌人,高级工程师,博士研究生,研究方向:导弹先进控制理论及作战使用。

收稿日期: 2011-03-06

  网络出版日期: 2025-05-30

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The Design and Simulation of Three Dimensional Self Calibration Guidance Law

  • CHEN Shengqi ,
  • ZHOU Jun
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  • Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2011-03-06

  Online published: 2025-05-30

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摘要

文中以变结构控制理论为基础,针对空对地攻击的模式提出了三维制导律。文中主要研究了测量误差和制导误差之间的关系,为了便于该三维制导律的工程应用,对其进行了改进。改进后的制导律的性能通过仿真和传统的比例导引律进行了对比,结果验证了所修改的制导律的合理性和可行性。

关键词： 测量误差; 制导误差; 三维制导律; 变结构控制

本文引用格式

陈胜琪 , 周军 . 三维自校正制导律的设计与仿真[J]. 弹箭与制导学报, 2011 , 31(6) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2011.06.033

Abstract

In this paper, a kind of three-dimensional guidance law for the air-to-surface attacking mode was derived based on the variable structure control (VSC) theory, then the relationship between the measurement error and guidance error was investigated and discussed thoroughly, the 3-D guidance law based on VSC was modified for easy implementation, the performance of modified guidance law was validated through the comparison between traditional guidance law and modified guidance law based on the computer simulation.

Key words： measurement error; guidance error; 3-D guidance law; variable structure control

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参考文献

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